NORSAT 4, 62702
Orbit data source: Space-Track
NORSAT 4, 62702 is a payload satellite owned by NSC (NO) in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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62702 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
NO / NORRelated business
Manufacturer
UTIAS-SFL
Mission
Operational Civil Com/Tech
Bus & Motor
DEFIANT, Unknown motor
Mass
35 kg wet, 35 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.6 m
Radar Cross Section
0.165 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 NORSAT 4
1 62702U 25009CX 26034.63089474 .00003379 00000-0 31863-3 0 9995
2 62702 97.7153 115.6766 0003052 111.8358 248.3187 14.94444583 57416Epoch: 2026-02-03T15:08Z
TLE epoch observation values (Epoch: 2026-02-03T15:08:29.305Z)
Latitude
-0.00005°
Longitude
114.74544°
Altitude
587.93 km
Speed
7.566 km/s
True Right ascension
07h 42m 42s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
13:02:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.235 km
Perigee altitude
578.987 km
Semi-major axis
6,959.248 km
Eccentricity
0.00031
Inclination
97.7153°
RAAN
115.6766°
Arg. of periapsis
111.8358°
True anomaly
248.28621°
Mean anomaly
248.3187°
Eccentric anomaly
248.30245°
Mean motion
3.73852 °/min
Orbital period
96.29 mins
BSTAR
0.00031863
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Other satellites on launch #9 in the year 2025 (2025-01-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.NORSAT 4 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-04 17:25:40.529Z | 40.329° NE | 2026-02-04 17:28:40.529Z | 90.603° ESE | 23.533° | 2026-02-04 17:31:40.529Z | 147.378° SSE |
| 4 mins | 2026-02-04 19:02:40.529Z | 322.287° NNW | 2026-02-04 19:03:40.529Z | 302.375° NW | 21.272° | 2026-02-04 19:06:40.529Z | 245.56° WSW |
| 6 mins | 2026-02-05 05:50:40.529Z | 205.803° SW | 2026-02-05 05:52:40.529Z | 251.501° W | 30.979° | 2026-02-05 05:56:40.529Z | 330.086° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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